The details of a study to develop accurate and efficient numerical schemes to predict complex flows are described. In this program, several discretization schemes were evaluated using simple test cases. This assessment led to the selection of three schemes for an in-depth evaluation based on two-dimensional flows. The scheme with the superior overall performance was incorporated in a computer program for three-dimensional flows. To improve the computational efficiency, the selected discretization scheme was combined with a direct solution approach in which the fluid flow equations are solved simultaneously rather than sequentially
Critical to the advancement of computational aerodynamics capability is the ability to simulate flow...
A procedure is presented for effective consideration of viscous effects in computational development...
The objective of this study was to develop a high-resolution-explicit-multi-block numerical algorith...
The objective of this effort is to develop improved numerical schemes for predicting combustor flow ...
The main objective of the NASA sponsored Aerothermal Modeling Program, Phase 2--Element A, is to dev...
The hybrid-upwind finite difference schemes employed in generally available combustor codes possess ...
An algorithm for laminar and turbulent viscous compressible two dimensional flows is presented. For ...
The flow field in and around the nozzle afterbody section of a hypersonic vehicle was computationall...
A numerical algorithm and computer program are presented for solving the laminar, transitional, or t...
A computer implemented numerical method for predicting the flow in and about an isolated three dimen...
A numerical scheme has been developed to solve the incompressible, 3-D Navier-Stokes equations using...
Convection effect and source terms are two primary sources of difficulties in computing turbulent re...
A general, user oriented computer program, called VNAF2, developed to calculate high Reynolds number...
Nowadays, in spite of disadvantages of turbulence closure models for RANS (Reynolds Averaged Navier-...
The capabilities of an existing 3-D incompressible Navier-Stokes flow solver, INS3D, are extended an...
Critical to the advancement of computational aerodynamics capability is the ability to simulate flow...
A procedure is presented for effective consideration of viscous effects in computational development...
The objective of this study was to develop a high-resolution-explicit-multi-block numerical algorith...
The objective of this effort is to develop improved numerical schemes for predicting combustor flow ...
The main objective of the NASA sponsored Aerothermal Modeling Program, Phase 2--Element A, is to dev...
The hybrid-upwind finite difference schemes employed in generally available combustor codes possess ...
An algorithm for laminar and turbulent viscous compressible two dimensional flows is presented. For ...
The flow field in and around the nozzle afterbody section of a hypersonic vehicle was computationall...
A numerical algorithm and computer program are presented for solving the laminar, transitional, or t...
A computer implemented numerical method for predicting the flow in and about an isolated three dimen...
A numerical scheme has been developed to solve the incompressible, 3-D Navier-Stokes equations using...
Convection effect and source terms are two primary sources of difficulties in computing turbulent re...
A general, user oriented computer program, called VNAF2, developed to calculate high Reynolds number...
Nowadays, in spite of disadvantages of turbulence closure models for RANS (Reynolds Averaged Navier-...
The capabilities of an existing 3-D incompressible Navier-Stokes flow solver, INS3D, are extended an...
Critical to the advancement of computational aerodynamics capability is the ability to simulate flow...
A procedure is presented for effective consideration of viscous effects in computational development...
The objective of this study was to develop a high-resolution-explicit-multi-block numerical algorith...